Fluid-structure interaction characteristics of inflatable reentry aeroshell at subsonic speed-Reference-Cited by-同舟云学术

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Fluid-structure interaction characteristics of inflatable reentry aeroshell at subsonic speed

Published:2023-02 Issue: Volume:133 Page:108112
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Saha Sanjoy Kumar^ORCID,Tobari Junki,Takahashi Yusuke^ORCID,Oshima Nobuyuki,Moriyoshi Takahiro,Yamada Kazuhiko,Shibata Ryoichi

Funder

University of Alberta

Japan Society for the Promotion of Science

Japan Aerospace Exploration Agency

Institute of Space and Astronautical Science

Hokkaido University

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference40 articles.

1. Hypersonic Inflatable Aerodynamic Decelerator (HIAD) technology development overview;Hughes,2011

2. Ballute aerocapture trajectories at Neptune;Lyons,2004

3. Supersonic inflatable aerodynamic decelerators for use on sounding rocket payloads;Miller,2014

4. Ultra lightweight ballutes for return to Earth from Moon;Masciarelli,2006

5. Static aeroelastic analysis of thin-film clamped ballute for Titan aerocapture;Rohrschneider;J. Spacecr. Rockets,2008

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Implementation of concavity over heat shield of a reentry vehicle in reducing aerodynamic heating;International Journal of Heat and Fluid Flow;2024-07

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